383534-2-2

38353422 Engine Gas Turbine Starter

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Datasheet. 383534-2-2 specification

Purchase Description Identification
The controlling activity and identification of a document used in lieu of a specification in the procurement of an item of supply.

99193-383534

Answers.

What is the NSN for 383534-2-2?

2995-01-326-2419

How is this classified for shipping?

Schedule B number: 8411997050
Parts of gas turbine aircraft engines, other than for use in civil aircraft

What's the federal classification of 383534-2-2?

FSC 2995 ⁓ Miscellaneous engine accessories, aircraft

Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.

Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).

NSN 2995-01-326-2419 STARTER,ENGINE,GAS TURBINE

NIIN
013262419
NIIN Date
09/21/90
Schedule B
8411997050 
Name Code
21907
FIIG
A23900
DEMIL / ITAR
USML/ITAR controlled item (Code: B)
Hazmat
No hazard information available from HMIRS.
MSDS
N/A
Precious Metals
Metal content unknown
Enviromental
N/A
Electrostatic ESD & EMI
No ESD or EMI sensitivity

Major End Users Countries and entities

  • - Brazil 
  • - Belgium 
  • - Italy 
  • - Nato Maintenance And Supply Agency 

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Similar by Design Other starters with similar characteristics

Nothing similar to this part number was found in our inventory

383534-2-2 / Starter,engine,gas turbineWhat is the formal definition of this item?

An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. the combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. may have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.